|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-007/04 B64D-033/02 F01D-021/04 F01D-025/24|
|우선권정보||FR-12 61166 (2012-11-23)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 11|
An aircraft nacelle comprising a first duct secured to an air intake and a second duct secured to a powerplant, the first duct comprising an exterior surface and an end portion connected to the second duct. The nacelle includes a hollow section piece in contact with the exterior surface of the first duct which extends over at least part of the circumference of that end portion of the first duct that is connected to the second duct.
1. An aircraft nacelle comprising: a first duct extending from an air intake of the aircraft nacelle to an end portion with a first duct annular ring flange extending away from an exterior surface of the first duct;a second duct surrounding a powerplant and having a first end including a second duct annular ring flange fastened to the first duct annular ring flange, wherein the first duct annular ring flange and the second duct annular ring flange both run in planes that are substantially perpendicular to a longitudinal direction;a hollow section piece c...